Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Cessna Citation Xls vs Daher Tbm 960
The Airbus H225 is a large twin‑engine helicopter, best suited to offshore, search‑and‑rescue, or utility missions. Its range is comparatively short versus fixed‑wing aircraft (typically a few hundred nautical miles, depending on payload and reserves), but it can carry a relatively high passenger load for rotorcraft, commonly around 16–19 in transport layouts (more in high‑density configurations). The Boeing BBJ MAX 9 is a long‑range VIP airliner based on the 737 MAX 9. It sits in the large‑cabin category with intercontinental-range capability (roughly 5,000+ nautical miles depending on configuration) and offers the greatest passenger capacity of the four, from a small VIP complement up to airline-style seating in the hundreds. The Cessna Citation XLS+ is a midsize business jet. It trades ultimate range for flexibility and runway performance, typically flying about 2,000 nautical miles and carrying about 7–9 passengers in standard executive seating. The Daher TBM 960 is a single‑engine turboprop in the very light business/travel category, usually seating 4–6 passengers with a range roughly in the 1,400–1,700 nautical mile class.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Cessna Citation XLS+ | Daher TBM 960 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 5.34 | $ 2.25 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 12 | 10 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Cessna Citation | Daher TBM |
| Aircraft Name | H225 | BBJ MAX 9 | XLS+ | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1906 | 1730 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.67 | $ 0.56 |
| Max Cabin Seats | 28 | 35 | 9 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | 7540 | 2908 |
| Standard Cabin Seats | 19 | 8 | 8 | 4 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 2,303 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 470 | 430 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $15,500,000 | $4,450,000 |
| Aircraft Type | — | — | — | Turbo Prop |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 10 | 10 | 6 |
| Max Cabin Seats | 28 | 35 | 9 | — |
| Standard Cabin Seats | 19 | 8 | 8 | 4 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 9.3 | 6.2 |
| SL Cabin Altitude (ft) | — | 24000 | 25230 | 14390 |
| Lavatory | — | — | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | AFT | — |
| Galley / Refreshment | — | — | Galley | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | PW545C | TBM 960 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 | 3500 |
| Horsepower | 2100 | — | — | 850 |
| No. of Engines | 2 | 2 | 2 | — |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | ISA + 49 |
| Thrust (lbs) | — | 28000 | 4119 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 52.5 | 35.3 |
| Overall Height (ft) | 16.3 | 40.3 | 17.2 | — |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 123 |
| Wingspan (ft) | — | 117.9 | 56.3 | 42.1 |
| Aisle Step (ft) | — | Flat Floor | 0.7 | — |
| Cabin Width (ft) | — | 11.6 | 5.5 | 4 |
| Cabin Height (ft) | — | 7.1 | 5.7 | 4.1 |
| Cabin Length (ft) | — | 107.2 | 18.5 | 13.4 |
| Cabin Width - Floor (ft) | — | 10.7 | 3.9 | — |
| Cabin Length - Seating (ft) | — | 100.6 | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | 80 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | — |